P/N: 3101524-6
Category: Turbine Engine Parts
This product requires a custom quote. Please contact our sales team for pricing information or submit an RFQ (Request for Quote).
| Condition | Stock |
|---|---|
| Serviceable | 1 Available |
The 3101524-6 is a combustor transition liner for gas turbine engines, directing hot combustion gases from the combustor liner to the turbine nozzle guide vanes. Constructed from high-temperature alloy material to withstand extreme thermal gradients and pressure pulses during engine operation. This component seats between the combustor liner and nozzle assembly, forming a critical interface in the engine's hot section.
Installation requires proper alignment and torque sequencing per engine maintenance manual specifications and FAA-approved data. Used in commercial and industrial gas turbine applications where reliable thermal management is essential.
Please note: Product descriptions are provided for informational purposes. Always refer to your aircraft's Illustrated Parts Catalog (IPC) to verify part compatibility and specifications.
The 3101524-6 is a combustor transition liner for gas turbine engines, directing hot combustion gases from the combustor liner to the turbine nozzle guide vanes. Constructed from high-temperature alloy material to withstand extreme thermal gradients and pressure pulses during engine operation.
The 3101524-6 is currently available in the following conditions: Serviceable. Each condition reflects the part's maintenance history and certification status per FAA standards.
The 3101524-6 requires a custom quote. Submit a Request for Quote (RFQ) through our website or call our sales team at (904) 998-9101 for immediate pricing assistance.
Yes, we offer same-day processing on in-stock items and provide 24/7 AOG (Aircraft on Ground) support for urgent needs. Standard, expedited, and overnight shipping options are available.